Minimum-Fuel Low-Earth-Orbit Aeroglide and Aerothrust Aeroassisted Orbital Transfer Subject to Heating Constraints | Zendy

Reagan Fuhr | Zendy; Anil V. Rao | Zendy

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Minimum-Fuel Low-Earth-Orbit Aeroglide and Aerothrust Aeroassisted Orbital Transfer Subject to Heating Constraints

Author(s) -

Reagan Fuhr,

Anil V. Rao

Publication year - 2018

Publication title -

journal of spacecraft and rockets

Language(s) - English

Resource type - Journals

SCImago Journal Rank - 0.758

H-Index - 79

eISSN - 1533-6794

pISSN - 0022-4650

DOI - 10.2514/1.a34073

Subject(s) - orbital maneuver , spacecraft , fuel efficiency , trajectory optimization , control theory (sociology) , thrust , optimal control , orbital elements , orbit (dynamics) , trajectory , phase (matter) , heat transfer , aerospace engineering , mechanics , physics , computer science , mathematics , engineering , mathematical optimization , control (management) , quantum mechanics , astronomy , artificial intelligence , astrophysics

A numerical optimization study of minimum-fuel low-Earth-orbit aeroglide and aerothrust aeroassisted orbital transfer of a small spacecraft subject to constraints on heating rate and heating load w...

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